IABSA Premier 64-01
| IABSA Premier 64-01 | |
|---|---|
| Type: | Light aircraft |
| Design country: | |
| Manufacturer: | |
| First flight: |
circa 1960 |
The IABSA Premier 64-01 was a multipurpose aircraft produced by the Brazilian manufacturer Industria Aeronáutica Brasileira .
construction
The Premier 64-01 was a stripped shoulder wing aircraft with a fixed tail wheel landing gear and a conventional tail unit. The cabin was accessible from the right side and the seats were one behind the other. The aircraft was powered by a Continental A75 boxer engine with 56 kW. The machine was only produced in small numbers.
Technical specifications
| Parameter | Data |
|---|---|
| crew | 1 |
| Passengers | 1 |
| length | 6.70 m |
| span | 10.70 m |
| height | ? |
| Wing area | 16 m² |
| Empty mass | 340 kg |
| Max. Takeoff mass | 580 kg |
| Cruising speed | 130 km / h |
| Top speed | 160 km / h |
| Service ceiling | 4000 m |
| Range | 600 km |
| Engines | 1 × Continental A75 boxer engine with 56 kW |
See also
literature
- John WR Taylor: Jane's All The World's Aircraft 1965-66 . Sampson Low, Marston & Company, London 1965
- The Illustrated Encyclopedia of Aircraft (Part Work 1982-1985) . Orbis Publishing.